N327NV

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 54,269 hrs · 38,425 cycles

(AIRCRAFT NOT GROUNDED) BATTERY FAILED EPSU SYSTEM TEST. / REMOVED AND REPLACED EPSU REF WO534775"

Part: POWER SUPPLY — FAULTED (ZONE 200) · airframe 53,984 hrs · 38,258 cycles

(AIRCRAFT NOT GROUNDED) EMERGENCY LIGHT RELATED TO ESPU FLICKERING / REMOVED AND REPLACED EPSU"

Part: BATTERY — NO TEST (ZONE 200) · airframe 53,588 hrs · 38,042 cycles

(AIRCRAFT NOT GROUNDED) FAILED EPSU BATTERY TEST / REMOVED AND REPLACED EPSU BATTERY REF WO 522931"

Part: OXYGEN BOX — NO TEST (ZONE 200) · airframe 53,421 hrs · 37,935 cycles

(AIRCRAFT NOT GROUNDED) TEST RESET BUTTON ON JUMPSEAT O2 BROKEN / REMOVED AND REPLACED PRIMARY OBSERVER'S O2 MASK STOWAGE BOX IAW AMM 35-12-41-000-001-A, AND 35-12-41-400-001-A. OPS TEST GOOD OK FOR SERVICE. THIS CLEARS MEL 25-11-06-A, MDDR# 211934. PLACARDS REMOVED.

Part: SLIDE — FAULTED (LT DOOR) · airframe 51,211 hrs · 36,795 cycles

CLASS 1 AFT LEFT ESCAPE SLIDE LIGHT FAULT WHILE PERFORMING EMERGENCY LIGHTING TEST. / PERFORMED TROUBLESHOOTING IAW TSM 25-62-00-810-078-B. REMOVED AND REPLACED L2 DOOR SLIDE IAW AMM 25-62-44-000-002. OPS CHECK GOOD, NO FURTHER DEFECTS NOTED. OK FOR SERVICE"

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 51,211 hrs · 36,795 cycles

EPSU BATTERY 10WL FAILED DURING EMERGENCY LIGHTING CHECK. / REMOVED AND REPLACED EPSU BATTERY 10WL IAW AMM 33-51-38-000-002-A & AMM 33-51-38-400-001-A."

Part: BATTERY — EXPIRED (AFT MEGAPHONE) · airframe 51,128 hrs · 36,756 cycles

AFT MEGAPHONE BATTERIES EXP / REPLACED BATTERIES IN AFT MEGAPHONE BATTERIES IAW AMM 25-65-51-920-001-A"

Part: EPSU — UNKNOWN (UNKNOWN) · airframe 50,423 hrs · 36,385 cycles

EMERGENCY LIGHT OPERATIONAL TEST FAILED: AFT EPSU (13WL) BAT FAULT. / AFT EPSU (13WL) REPLACED AND TESTED SERVICEABLE IAW AMM 33-51-38-000-001-A / 400-001-A."

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 50,420 hrs · 36,383 cycles

RH WING TRAILING EDGE OVERHANG AREA, CORROSION FOUND AT LOWER SURFACE OF TOP SKIN BTW RIB 16 TO WMRX 5855.60. / RH WING TRAILING EDGE OVERHANG AREA TOP SKIN LOWER SURFACE BTW RIB 16 TO WMRX 5855.60, CORROSION REMOVED AND FOUND STRUCTURALLY ACCEPTABLE AS PER AIRBUS DOSSIER # 81283571. PERMANENTLY DISPOSITION PERFORMED AS PER REPAIR INSTRUCTIONS R572-58616 ISSUE L PARAGRAPH D AND E ( SEPT-05-2022 ) AND COMPLY ALLEGIANT ERO # R5721-0151 REV 00. REPAIRED CLASSIFIED MAJOR CATEGORY B WITH FUTURE INSPECTIONS AS PER RDAF # 81283571/002/2023#A. THRESHOLD INSPECTIONS: 31 000FC / 57 000FH, INTERVAL INSPECTIONS: 31 000FC / 57 000FH AND METHOD OF INSPECTION: EXTERNAL DETAILED VISUAL INSPECTION. SEE AWS FOR DETAILS OF WORK ACCOMPLISHED, NDT REPORT MWO: 55907-15 AND ATTACHED SHEETS FOR RESULTS. 990001287"

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 50,420 hrs · 36,383 cycles

LH WING, SPOILER NO.5, CENTER HINGE FITTING, ANTI-ROTATION WEB FOUND GAUGE. / L/H WING, SPOILER NO 5, CENTER HINGE FITTING, ANTI-ROTATION WEB PERMANENTLY REPAIRED AS PER SRM 57-70-00-300-004 REV 145 AND COMPLY AS PER SRM57-70-00-300-003 REV 145 FIG 001. THIS REPAIR TASK IS CATEGORY A WITH NO FURTHER ACTION REQUIRED. SEE AWS FOR DETAILS AND NDT REPORT MWO: 55907-12. BOLT P/N: D5774507120000, PO#: 2038322. NUT P/N: MS21042-3, PO#: 2034243. NUT P/N: NSA5454-12RH01, PO#: 1799404. BOLT P/N: NAS1303-51, PO#: 1677237. STAINLESS P/N: 17-4PH .O63IN, PO#: 1569232."

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 50,423 hrs · 36,385 cycles

LH WING SLAT #3 UPPER SKIN INBD SIDE, DAMAGE FOUND / LH WING SLAT #3 UPPER SKIN INBD SIDE REPAIRED AS PER SRM 57-44-21-300-011 REV 145. SEE AWS FOR ADDITIONAL WORK DETAILS. THIS IS MAJOR REPAIR CAT A. NO FURTHER ACTION REQUIRED."

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 50,420 hrs · 36,383 cycles

LH WING SLAT #3 UPPER SKIN INBD SIDE, DAMAGE FOUND. / LH WING SLAT #3 UPPER SKIN INBD SIDE REPAIRED AS PER SRM 57-44-21-300-011 REV 145. SEE AWS FOR ADDITIONAL WORK DETAILS. THIS IS MAJOR REPAIR CAT A. NO FURTHER ACTION REQUIRED."

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 50,420 hrs · 36,383 cycles

RH WING TRAILING EDGE OVERHANG AREA, CORROSION FOUND AT LOWER SURFACE OF TOP SKIN BTW WMRX 4784.32 TO RIB 16. / RH WING TRAILING EDGE OVERHANG AREA TOP SKIN LOWER SURFACE BTW WMRX 4784.32 TO RIB 16, CORROSION REMOVED AND FOUND STRUCTURALLY ACCEPTABLE AS PER AIRBUS DOSSIER # 81283571. PERMANENTLY DISPOSITION PERFORMED AS PER REPAIR INSTRUCTIONS R572-58616 ISSUE L PARAGRAPH D AND E ( SEPT-05-2022 ) AND COMPLY ALLEGIANT ERO # R5721-0151 REV 00. REPAIRED CLASSIFIED MAJOR CATEGORY B WITH FUTURE INSPECTIONS AS PER RDAF # 81283571/002/2023#A. THRESHOLD INSPECTIONS: 31 000FC / 57 000FH, INTERVAL INSPECTIONS: 31 000FC / 57 000FH AND METHOD OF INSPECTION: EXTERNAL DETAILED VISUAL INSPECTION. SEE AWS FOR DETAILS OF WORK ACCOMPLISHED, NDT REPORT MWO: 55907-7 AND ATTACHED SHEETS FOR RESULTS. M313 - CONTROL #990001286"

Part: BATTERY — INOPERATIVE · airframe 48,814 hrs · 35,505 cycles

NRC 7000-0011: DURING EMERGENCY BITE TEST, FOUND BATTERY FROM EPSU 10 WL AND 13WL INOP. TO BE REPLACED. / BATTERIES FROM EPSU 10WL AND 13WL REPLACED AND TESTED SERVICEABLE IAW AMM 33-51-38-000-002-A/400-002-A."

Part: BULB — INOPERATIVE · airframe 48,814 hrs · 35,505 cycles

NRC 7000-0010: ON LH OVERWING BODY FAIRING, FWD EMERGENCY LIGHT, AFT BULB FOUND INOP. TO BE INVESTIGATED. / ON LH OVERWING BODY FAIRING, FWD EMERGENCY LIGHT, AFT BULB RE-INSTALLED PROPERLY AND TESTED SERVICEABLE IAW AMM 33-51-15-400-001-A."

Part: NONE — NONE · airframe 48,799 hrs · 35,498 cycles

REF LP 1471030 MAINT REINSPECT REQUIRED FOR OUT STATION MAINTENANCE L1 DOOR LOWER EMERGENCY EXIT LLIGHT LENS BROKE OFF / PERFORMED MAINT REINSPECT OF OUTSTATION MAINTENANCE ON L1 DOOR LOWER EMERGENCY EXIT LIGHT LENS. REPLACED EMERGENCY EXIT LIGHT LENS IAW AMM 33-51-13. THIS SATIFIES PROCEDURES OF M313 05330002/1 AND M313 05330002/2"

Part: PLUG — DIRTY · airframe 48,710 hrs · 35,452 cycles

CABIN EMERGENCY LIGHT FAULTED BAT/EPSU (13WL) AFT L/H. / REMOVED CANON PLUG CLEANED AND REINSTALLED ON EPSU 13WL , OPS CHECK GOOD AS PER AMM 33-51-38-420-050-A."

Part: EPSU — NONE · airframe 48,533 hrs · 35,362 cycles

DURING BATTERY CHECK MCDU DISPLAYS 11-WL BATTERY FAIL. / REPLACED EMERGENCY LIGHT BATTERY (11WL) PER AMM 33-51-38 P/B 401. PERFORMED OPS TEST PER WORK CARD."

Part: EPSU — NONE · airframe 48,494 hrs · 35,342 cycles

PERFORMED EMERGENCY LIGHT TEST AND FOUND RIGHT EPSU BATT FAULTING / REMOVED AND REPLACED RIGHT EPSU BATT. OPS CHECKS GOOD IAW AMM 33-51-38 PB 401"

Part: BATTERY — LOW · airframe 47,927 hrs · 35,010 cycles

LEFT SIDE OVER WING EMERGENCY EXIT LIGHT NOT ILLUMINATING. / T/S & FOUND EMERG. LIGHT OVER LH ESCAPE EXITS (WING) DIMLY LIT. R&R'D BATTERY AT 11WL, NO FIX. RE-INSTALLED ORIG. BAT. REMOVED & CLEANED CANNON PLUG OF EPSU AT 11WL & LIGHT IS WORKING NORMAL. REF A319 AMM 33-51-38 PB401."

Part: LIGHT — INOPERATIVE · airframe 47,601 hrs · 34,826 cycles

LT WING EXTERIOR EMERG EXIT LIGHTS INOP. / RELAMPED LT WG EXT EMERG EXIT LIGHTS AND OPS CK GOOD REF AMM 33-51-16."

Part: EPSU — FAILED · airframe 47,601 hrs · 34,826 cycles

EPSU TEST FAILS 11WL. / REMOVED AND REPLACED 11WL EPSU AND BATT PACK OPS CK GOOD REF AMM 33-51-38 PB401. NO FAULTS NOTED AND TEST OK."

Part: NONE — CORRODED (ZONE 600) · airframe 47,515 hrs · 34,783 cycles

DURING A VISUAL INSPECTION PER TASK CARD Nº: 572066-01-1-002, IT WAS FOUND AT RH WING T/E FALSE REAR SPAR OVERHANG AREA, BETWEEN RIB 6 AND RIB 9 THE UPPER SKIN LOWER SURFACE WITH CORROSION. DUE THIS FACT DETAILS WERE SENT TO AIRBUS ASKING FOR REPAIR INSTRUCTIONS AND FINAL APPROVAL, UNDER DOSSIER 80979038 AND COOPESA COO-EO-2021-14099-R001

Part: NONE — CORRODED (ZONE 500) · airframe 47,515 hrs · 34,783 cycles

DURING A VISUAL INSPECTION PER TASK CARD Nº: 572054-02-1-001_P1-OP-UP/0, IT WAS FOUND AT LH WING - BOTTOM SKIN PANEL 2, LOWER SURFACE, RIBS 1-2, FUEL PUMP SURROUND. DUE THIS FACT DETAILS WERE SENT TO AIRBUS ASKING FOR REPAIR INSTRUCTIONS AND FINAL APPROVAL, UNDER DOSSIER 80984144 AND GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO. COOPESA COO-EO-2021-14273 . FOR ADDITIONAL DETAILS SEE COOPESA JOB A1K273 ITEM 5-24

Part: STRUCTURE — CORRODED (ZONE 100) · airframe 47,515 hrs

DURING A VISUAL INSPECTION PER TASK CARD Nº: 534107-01-1-001_PL-OP-UP/0), IT WAS FOUND AT ,SECTION 16/17, AFT CARGO COMPARTMENT AT STRG-39R LEVEL BETWEEN FR 55A AND FR59 LOWER DOOR SILL UPPER FLANGE AND ATTACHED FITTINGS WITH CORROSION. DUE THIS FACT DETAILS WERE SENT TO AIRBUS ASKING FOR REPAIR INSTRUCTIONS AND FINAL APPROVAL, UNDER DOSSIER 80984059 AND GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO. COOPESA COO-EO-2021-14321. FOR ADDITIONAL DETAILS SEE COOPESA JOB A1K273 ITEM 1-100

Part: NONE — CORRODED (ZONE 500) · airframe 47,515 hrs · 34,783 cycles

DURING A VISUAL INSPECTION PER TASK CARD Nº: 572066-01-1-002, IT WAS FOUND AT LH WING T/E FALSE REAR SPAR OVERHANG AREA, BETWEEN RIB 6 AND RIB 9 THE UPPER SKIN LOWER SURFACE WITH CORROSION. DUE THIS FACT DETAILS WERE SENT TO AIRBUS ASKING FOR REPAIR INSTRUCTIONS AND FINAL APPROVAL UNDER DOSSIER 80980133 AND COOPESA COO-EO-2021-14098-R001

Part: NONE — NONE (ZONE 700) · airframe 47,515 hrs

DURING A VISUAL INSPECTION PER ALLEGIANT CARD NO 53-140-002 , IT WAS FOUND AT MLG DOOR ACTUATOR FITTING ON KEEL BEAM RH AND LH SIDE. DUE THIS FACT DETAILS WERE SENT TO ALLEGIANT ASKING FOR REPAIR INSTRUCTIONS AND FINAL APPROVAL, UNDER ALLEGIANT ERO NUMBER R5336-0012 REV 00 AND R5336-0011 REV 00 GUIDELINES . FOR ADDITIONAL DETAILS SEE COOPESA JOB A1K273 ITEM 1-55 AND ITEM 1-54

Part: NONE — CORRODED (ZONE 500) · airframe 47,515 hrs

DURING A VISUAL INSPECTION PER TASK CARD Nº: TASK CARD ZL-500-03 (EWIS), IT WAS FOUND AT ,LH WING, UPPER SKIN UPPER SURFACE CORRODED AT STRG-11 BETWEEN RIB 6 AND RIB 9.. DUE THIS FACT DETAILS WERE SENT TO AIRBUS ASKING FOR REPAIR INSTRUCTIONS AND FINAL APPROVAL, UNDER DOSSIER 70584307 AND GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO. COOPESA COO-EO-2021-14208 R01 . FOR ADDITIONAL DETAILS SEE COOPESA JOB A1K273 ITEM 5-52

Part: FRAME — CORRODED (ZONE 100) · airframe 47,515 hrs · 34,783 cycles

DURING A VISUAL INSPECTION PER TASK CARD NO 534107-01-1-001_P1-OP-UP/0, IT WAS FOUND AT AFT CARGO COMPARTMENT AT FR59 BETWEEN STGR 35RH AND STGR 44 INBD UPPER FLANGE WITH CORROSION AND VERTICAL FLANGE BETWEEN STGR 41RH AND STGR 43RH WITH EXISTING REWORK.. DUE THIS FACT DETAILS WERE SENT TO AIRBUS ASKING FOR REPAIR INSTRUCTIONS AND FINAL APPROVAL, UNDER DOSSIER NUMBER 80982397 GUIDELINES . FOR ADDITIONAL DETAILS SEE COOPESA ENGINEERING ORDER NO COO-EO-2021-14185 ,JOB A1K273 ITEM 1-92

Part: EPSU — FAILED (CABIN) · airframe 46,931 hrs · 34,483 cycles

REF NR 794471 CIDS1 EPSU SYS TEST FAILS AND DISPLAYS ESCAPE SLIDE LT/EPSU (10WL) FWD L MESSAGE CLASS 1; REQUIRES FURTHER TROUBLESHOOTING. / REPIN WIRE 5109 PIN B CONNECTOR 2871VC L DOOR SLIDE. OP TEST EPSU SYSTEM OK W/REF TSM 25-60-00-810-811A, ESPM 20-*48-14-01 & ASM 33-51-01 PG 0387."

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 45,710 hrs · 33,847 cycles

EPSU BATTERIES 10WL, 11WL, 12WL FAILED CABIN EMERGENCY LIGHTING CAPACITANCE TEST. REPLACED ALL 3 EPSU BATTERIES 10WL, 11WL, 12WL W/REF TO AMM 33-51-38 PB 401. OPERATIONS CHECK GOOD. OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,241 hrs · 33,572 cycles

DURING EPSU BATTERY TEST EPSU 13WL BATTERY FAULT LIGHT ILLUMINATED. REMOVED AND REPLACED EPSU 13WL BATTERY REF AMM 33-51-38 PB401. OPS CHECKED GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 44,429 hrs · 33,132 cycles

EMERGENCY DECLARED) ON APPROACH RECEIVED ECAM F/CTL FLAPS FAULT / REPLACED FLAP-PCU"

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 42,066 hrs · 31,985 cycles

EPSU 12WL FAILED AN EMERGENCY LIGHT CHECK. R & R THE EPSU.

Part: STRIP — CORRODED (RT ELEVATOR)

RIGHT ELEVATOR CONDUCTIVE STRIP CORRODED AND CRACKED

Part: BUSHING — OUT OF LIMITS (LT ELEVATOR)

LEFT ELEVATOR INBD AND OTBD ACTUATOR ATTACH BUSHINGS ON ELEVATOR SIDE OUT OF LIMITS.

Part: PIN — UNSECURE (CONNECTOR) · airframe 39,139 hrs · 30,522 cycles

L2 DOOR FLIGHT ATTENDANT OXYGEN MASK DOOR DOESN'T UNLATCH DURING MANUAL RELEASE CHECK. TROUBLESHOOT THE FLIGHT ATTENDANT OXYGEN MASK DOOR LATCH. FOUND PIN F ON 7227VT NOT SEATED. REINSTALLED THE PIN IAW AWM 35-23-06, P 0105, SHEET 1. OPS CHECKED GOOD IAW AMM 35-23-00-710-001-A.

Part: ACOUSTIC PANEL — CRACKED (NR 2 ENGINE) · airframe 35,153 hrs · 28,401 cycles

DURING DAILY CHECK WALK AROUND, DISCOVERED CRACKED ACOUSTIC PANEL AT 12 - 2 O'CLOCK POSITION ON NR 2 ENG. R & R ACOUSTIC PANEL AT 12 - 2 O'CLOCK POSITION IAW AMM 72-23-00. ALL IS GOOD.

Part: FAN — FAULTY (COCKPIT) · airframe 34,689 hrs · 28,221 cycles

DURING CRUISE FLIGHT AT FL 340, CREW FELT A VIBRATION FOLLOWED BY A STRONG FUME SMELL IN THE FLIGHT DECK THAT DRIFTED ALL THE WAY DOWN THE CABIN. DECLARED AN EMER WITH ATC & DIVERTED. ALL QRH CHECKLISTS WERE COMPLIED WITH. CREW HAD DONNED THEIR OXYGEN MASKS & ONCE DOWN OVER THE AIRPORT THE CAPTAIN NOTED THAT THE FUMES HAD DISSIPATED, BUT WERE STILL LINGERING IN THE FLIGHT DECK. ONCE ON THE GND THE CREW RECEIVED AN EXTRACT FAN FAULT ON THE ECAM. PERFORMED POST FLIGHT REPORT REVIEW & FOUND EXTRACT FAN 18HQ, PERFORMED A EVC TEST & HEAR EXTRACT FAN TO MAKE LOUD GRINDING NOISE. REPLACED EXTRACT FAN IAW AMM 21-26-51. OPERATES NORMAL CLEARED ECAM MSG, OK FOR SERVICE.